Powerplant (Engines) Flashcards

1
Q

Time limit for takeoff trust

A

5min

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2
Q

Maximum N1

A

106%

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3
Q

Maximum N2

A

105%

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4
Q

Max EGT takeoff

A

930 degrees C (940 degrees C 20sec transient)

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5
Q

Max cont EGT

A

895 degrees C

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6
Q

Max start

A

725 degrees C

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7
Q

Min oil psi

A

13

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8
Q

Max oil temp

A

165 degrees C

165-160 degrees C (15 min)

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9
Q

Max continuous oil temp

A

160 degrees C

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10
Q

Continuous engine ignition must be on for

A

Take off, landing and engine anti-ice on

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11
Q

Minimum start pneumatic psi

A

30 (- .5psi per 1000ft AMSL)

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12
Q

The PMC makes fuel flow adjustments to the MEC by monitoring

A
  • Thrust lever angle
  • Inlet Temp and pressure
  • N1 RPM
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13
Q

Thrust reverser light indicates

A
  • A disagreement between selector valve and isolation valve
  • If one or two reverser levers are not in the commanded position
  • Auto restow system has been activated
  • Any other time a malfunction has occurred
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14
Q

If the reverser light is on for more then 12sec what will illuminate

A

The MASTER CAUTION and ENG annunciation lights. The delay allows time for completion of the normal stowing cycle

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15
Q

What is PMC doing in the on position

A

The PMC is providing a signal to the MEC to modify N1 for better control of thrust settings (compensates for variations in inlet temp and pressure

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16
Q

Low idle light indicates

A

Insufficient engine RPM (less than 25% inflight)

17
Q

Low idle light is prevented from illuminating when

A
  • Air/ground logic senses on ground condition

- Engine start lever in cutoff position

18
Q

The PMC also provides

A
  • Smooth acceleration
  • minimal EGT overshoot
  • limited overspeed protection
19
Q

The PMC is powered by

A

The N2 speed sensor which is an AC generator

20
Q

With the PMC off during takeoff

A

Engine RPM may increase as speed increases (may be as much as 7%)

21
Q

The two idle speeds are

A

Low approx 22% N1

High approx 32% N1

22
Q

High idle is used when

A

For all stages of flight

23
Q

High idle switched to low idle

A

4 sec after touchdown (delay to enhance engine acceleration for reverse thrust)

24
Q

With a normal electrical failure the engine idle speed does what

A

Automatically goes to High idle (held in low idle with a solenoid)